发明名称 |
Rotor of an axial compressor stage of a turbomachine |
摘要 |
The present invention relates to a rotor of an axial compressor stage of a turbomachine featuring a rotor assembly with a rotary axis, forming on its circumference a blade ring with a radially outer ring surface, and several rotor blades arranged on the blade ring. It is provided that the ring surface between two adjacent rotor blades has at least in a partial area a changing radius relative to the rotary axis of the rotor assembly both in the axial direction and in the circumferential direction.
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申请公布号 |
US2012251324(A1) |
申请公布日期 |
2012.10.04 |
申请号 |
US201213431408 |
申请日期 |
2012.03.27 |
申请人 |
JOHANN ERIK;HEINICHEN FRANK;ROLLS-ROYCE DEUTSCHLAND LTD & CO KG |
发明人 |
JOHANN ERIK;HEINICHEN FRANK |
分类号 |
F01D5/02 |
主分类号 |
F01D5/02 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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